DAE-31 AIRFOIL

Thickness: 11.1%
Camber: 6.7%
Trailing edge angle: 7.0o
Lower flatness: 15.1%
Leading edge radius: 2.6%
Efficiency: 41.2
Max CL: 1.877
Max CL angle: 14.0
Max L/D: 58.83
Max L/D angle: 5.5
Max L/D CL: 1.287
Stall angle: -0.5
Zero-lift angle: -6.5